重复使用火箭着陆结构稳定性分析$^{\bf 1)}$
袁晗*,王小军†2)(
),张宏剑*3)(),石玉红*,张希*,章凌*
),张宏剑*3)(),石玉红*,张希*,章凌*
STABILITY ANALYSIS OF REUSABLE LAUNCH VEHICLE LANDING STRUCTURE$^{\bf 1)}$
Yuan Han*,Wang Xiaojun†2)(),Zhang Hongjian*3)(),Shi Yuhong*,Zhang Xi*,Zhang Ling*
),Zhang Hongjian*3)(),Shi Yuhong*,Zhang Xi*,Zhang Ling*
图1. 2-2 着陆模式的通用等效模型
Fig.1. Universal equivalent model of 2-2 landing mode
